 | This article needs additional citations for verification. Please help improve this article by adding citations to reliable sources. Unsourced material may be challenged and removed. Find sources: "Morane-Saulnier MoS-50" – news · newspapers · books · scholar · JSTOR (August 2017) (Learn how and when to remove this message) |
| MoS-50 | |
|---|---|
_K-SIM_02.jpg) Morane-Saulnier MS 50C at Aviation Museum of Central Finland | |
| General information | |
| Type | Trainer aircraft |
| Manufacturer | Morane-Saulnier |
| Primary users | French Air Force Finnish Air Force Turkish Air Force |
| History | |
| Introduction date | 1924 |
| Retired | 1930s |
Morane-Saulnier MoS-50 (also MS.50) was a French parasol configuration trainer aircraft built in 1924. The twin-seat aircraft was of wooden construction and was one of the last aircraft to have a rotary engine, a 97 kW (130 hp) Clerget 9B.
In 1925 six MS.50Cs were sold to Finland, where they were used as trainers until 1932. It was very popular in service. Five aircraft of the modified MS.53 type were sold to Turkey.
Versions
- Morane-Saulier M.S.50
- Three seat prototype, powered by a 89 kW (120 hp) Salmson AC9 9-cylinder radial engine.
- M.S.50C
- Two-seat primary trainer aircraft powered by a 97 kW (130 hp) Clerget 9B rotary engine.
- M.S.51
- Powered by a 130 kW (180 hp) Hispano-Suiza 8ab V-8 cylinder piston engine. Only three were built.
- M.S.53
- Improved version of M.S.51, with same engine.
- M.S.120
- M.S.53 with a 170 kW (230 hp) Salmson engine.
Survivors
The only preserved aircraft of this type is at the Aviation Museum of Central Finland.
Operators
Specifications (MS 50C)
Data from Thulinista Hornettiin
General characteristics
- Crew: 2
- Length: 7.6 m (24 ft 11 in)
- Wingspan: 11.7 m (38 ft 5 in)
- Height: 3.1 m (10 ft 2 in)
- Wing area: 24 m (260 sq ft)
- Max takeoff weight: 860 kg (1,896 lb)
- Powerplant: 1 × Clerget 9B 9-cyl air-cooled rotary piston engine, 100 kW (130 hp)
- Propellers: 2-bladed
Performance
- Maximum speed: 170 km/h (110 mph, 92 kn)
- Endurance: 2½ hours
- Service ceiling: 5,500 m (18,000 ft)
- Rate of climb: 2 m/s (390 ft/min)
See also
Related lists
References
- Serryer, J. (5 March 1925). "L'avion Morane, type 50". Les Ailes (194): 2.
- ^ Serryer, J. (20 May 1926). "Les avions Morane-Saulnier". Les Ailes (257): 2–3.
- Ogden, Bob (2009). Aviation Museums and Collections of Mainland Europe. Air Britain (Historians) Ltd. p. 93. ISBN 978 0 85130 418 2.
- Heinonen, Timo (1992). Thulinista Hornettiin - 75 vuotta Suomen Ilmavoimien koneita. Keski-Suomen Ilmailumuseon. ISBN 9519568824.
Further reading
- Lacaze, Henri & Lherbert, Claude (2013). Morane Saulnier: ses avions, ses projets [Morane Saulnier: Their Aircraft and Projects] (in French). Outreau, France: Lela Presse. ISBN 978-2-914017-70-1.